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Volumn 1, Issue , 2004, Pages 578-583

Towards design of mach 1.6+ cruise aircraft

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ASPECT RATIO; DRAG; FUEL CONSUMPTION; LIFT; REYNOLDS NUMBER; WINGS;

EID: 20744447188     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5070     Document Type: Conference Paper
Times cited : (4)

References (31)
  • 15
    • 20744445928 scopus 로고    scopus 로고
    • Vortex flow dilemmas & control on wing planforms for high speeds
    • Loen, Norway, May
    • NANGIA, R.K. & MILLER, A.S. "Vortex Flow Dilemmas & Control on Wing Planforms for High Speeds", RTO AVT Symposium, Loen, Norway, May 2001.
    • (2001) RTO AVT Symposium
    • Nangia, R.K.1    Miller, A.S.2
  • 23
    • 2942740195 scopus 로고    scopus 로고
    • Design of conventional & unconventional wings for UAV's
    • "UV for Aerial & Naval Military Operations" Ankara, Turkey, Oct.
    • NANGIA, "Design of Conventional & Unconventional Wings for UAV's", RTA-AVT Symposium, "UV for Aerial & Naval Military Operations", Ankara, Turkey, Oct. 2000.
    • (2000) RTA-AVT Symposium
    • Nangia1
  • 27
    • 2942742089 scopus 로고    scopus 로고
    • Developing an inverse design method using 3-D membrane analogy
    • NANGIA, R.K., "Developing an Inverse Design Method using 3-D Membrane Analogy", Future Paper.
    • Future Paper
    • Nangia, R.K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.